JPH07112835B2 - 航空機の操縦力勾配付与装置 - Google Patents

航空機の操縦力勾配付与装置

Info

Publication number
JPH07112835B2
JPH07112835B2 JP59032249A JP3224984A JPH07112835B2 JP H07112835 B2 JPH07112835 B2 JP H07112835B2 JP 59032249 A JP59032249 A JP 59032249A JP 3224984 A JP3224984 A JP 3224984A JP H07112835 B2 JPH07112835 B2 JP H07112835B2
Authority
JP
Japan
Prior art keywords
force gradient
steering force
signal
pitch
imparting device
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
JP59032249A
Other languages
English (en)
Japanese (ja)
Other versions
JPS59164297A (ja
Inventor
リチヤ−ド・デニス・マ−フイ−
ダグラス・ハロルド・クレルフオ−ド
Original Assignee
ユナイテッド・テクノロジ−ズ・コ−ポレイション
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by ユナイテッド・テクノロジ−ズ・コ−ポレイション filed Critical ユナイテッド・テクノロジ−ズ・コ−ポレイション
Publication of JPS59164297A publication Critical patent/JPS59164297A/ja
Publication of JPH07112835B2 publication Critical patent/JPH07112835B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0841Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability to prevent a coupling between different modes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Fluid-Driven Valves (AREA)
  • Compositions Of Oxide Ceramics (AREA)
JP59032249A 1983-02-22 1984-02-22 航空機の操縦力勾配付与装置 Expired - Fee Related JPH07112835B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/468,750 US4563743A (en) 1983-02-22 1983-02-22 Maneuver-force gradient system
US468750 1983-02-22

Publications (2)

Publication Number Publication Date
JPS59164297A JPS59164297A (ja) 1984-09-17
JPH07112835B2 true JPH07112835B2 (ja) 1995-12-06

Family

ID=23861080

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59032249A Expired - Fee Related JPH07112835B2 (ja) 1983-02-22 1984-02-22 航空機の操縦力勾配付与装置

Country Status (9)

Country Link
US (1) US4563743A (no)
JP (1) JPH07112835B2 (no)
AU (1) AU556414B2 (no)
DE (1) DE3406050C2 (no)
DK (1) DK80384A (no)
ES (1) ES8502652A1 (no)
GB (1) GB2135479B (no)
NO (1) NO158128C (no)
SE (1) SE450371B (no)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5170969A (en) * 1988-11-23 1992-12-15 The Boeing Company Aircraft rudder command system
US5001646A (en) * 1988-12-19 1991-03-19 Mcdonnell Douglas Corporation Automated helicopter flight control system
US5188511A (en) * 1991-08-27 1993-02-23 United Technologies Corporation Helicopter anti-torque device direct pitch control
US5213282A (en) * 1991-08-28 1993-05-25 United Technologies Corporation Maneuver feel system for a rotary wing aircraft
US5489830A (en) * 1994-09-09 1996-02-06 Mcdonnell Douglas Corporation Control system with loadfeel and backdrive
US7248949B2 (en) * 2004-10-22 2007-07-24 The Mitre Corporation System and method for stochastic aircraft flight-path modeling
DE102005055584B4 (de) * 2005-11-18 2009-04-09 Deutsches Zentrum für Luft- und Raumfahrt e.V. Steuerungseinrichtung und Verfahren zur Generierung von Steuerungssignalen für technische Vorrichtungen
US7784340B2 (en) * 2008-08-04 2010-08-31 Bell Helicopter Textron, Inc. Force gradient using a non-contact proximity sensor
CA2732671C (en) * 2008-08-04 2015-07-14 Bell Helicopter Textron, Inc. Force gradient using a non-contact proximity sensor
US10479491B2 (en) * 2017-08-17 2019-11-19 Textron Innovations Inc. System and method for rotorcraft collective power hold

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4067517A (en) * 1976-02-03 1978-01-10 United Technologies Corporation Automatic heading synchronization control system
US4261537A (en) * 1979-02-28 1981-04-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Velocity vector control system augmented with direct lift control
US4387432A (en) * 1981-03-30 1983-06-07 United Technologies Corporation Pulsed aircraft actuator
US4392203A (en) * 1981-03-30 1983-07-05 United Technologies Corporation Aircraft coordinated turn with lagged roll rate
US4387430A (en) * 1981-03-30 1983-06-07 United Technologies Corporation Pitch stick force inhibit of aircraft automatic outer loop
US4484283A (en) * 1981-03-30 1984-11-20 United Technologies Corporation Aircraft roll-yaw fault protocols

Also Published As

Publication number Publication date
SE8400953D0 (sv) 1984-02-21
US4563743A (en) 1986-01-07
JPS59164297A (ja) 1984-09-17
SE8400953L (sv) 1984-08-23
DK80384A (da) 1984-08-23
GB2135479A (en) 1984-08-30
DE3406050C2 (de) 1997-12-11
SE450371B (sv) 1987-06-22
GB8402940D0 (en) 1984-03-07
NO840608L (no) 1984-08-23
DE3406050A1 (de) 1984-08-23
NO158128B (no) 1988-04-11
ES529905A0 (es) 1985-01-16
ES8502652A1 (es) 1985-01-16
NO158128C (no) 1988-07-20
DK80384D0 (da) 1984-02-21
AU2451184A (en) 1984-08-30
AU556414B2 (en) 1986-10-30
GB2135479B (en) 1987-03-11

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Legal Events

Date Code Title Description
LAPS Cancellation because of no payment of annual fees